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Stabilization of satellite steady-state motions using moments arising from interaction with geomagnetic fieldстатья
- Авторы: Kalenova V.I., Morozov V.M., Rak M.G.
- Сборник: XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION
- Год издания: 2023
- Издательство: OAE Publishing Inc.
- Местоположение издательства: United States
- DOI: 10.1063/5.0108978
- Аннотация: A rigorous analytical approach to the problem of stabilizing steady-state motions (relative equilibrium and regular precessions) of a satellite, whose center of mass moves in a circular orbit, is presented. To create control torques, the satellite is equipped with magnetic coils and a screen with an electric charge. The essence of the approach is to use the property of reducibility of the original time-varying system to a time-invariant system. Controllability is investigated and correct algorithms for optimal stabilization are constructed. Their effectiveness has been shown.
- Добавил в систему: Муницына Мария Александровна